Numerical Study on the Atomization Characteristics of Double-Swirl Coaxial Injector
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3586
Reference17 articles.
1. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
2. ROLE OF GEOMETRIC PARAMETERS ON THE DROP SIZE CHARACTERISTICS OF LIQUID-LIQUID COAXIAL SWIRL ATOMIZERS
3. 4A.R. Ramezani and A. Ghafourian, "Spray angle variation of liquid-liquid swirl coaxial injectors". 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA2005-3747 (2005).
4. 5K. Ghorbanian, M.R. Soltani, M.R. Morad and M. Ashjaee. "Neural Network Prediction of a Liquid-Liquid Coaxial Swirl Injector Performance Map", 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2005-1430 (2005).
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